# STC SA1003CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Global Helicopters, Inc, United States
- Description: Replacement of Hughes P/N269A5501 idler pulley with Hughes P/N269A5414 idler pulley.
- Applied: June 20, 1973
- Status date: April 8, 1974
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS 4H12](https://openairdocs.org/tcds/4H12)
- Certificate PDF: https://openairdocs.org/files/sha256/c8/33/c8330ae84780bff15531237ea0a99e97f9657b3d4a15b6e5b3bc8407eff3ce2f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5627207B50ED454186257D3C0065E702.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1003CE

## ADs that name it (0)

None.

## Approved models (3)

- Sikorsky Aircraft Corporation 269A ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Sikorsky Aircraft Corporation 269A-1 ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Sikorsky Aircraft Corporation 269B ([TCDS 4H12](https://openairdocs.org/tcds/4H12))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

United gtatti of Slmtrira ©epartmcnt of transportation - federal SlOiation administration Supplemental Ttjipe Certificate i/uvm#€fr' 3A1U03CE Global Helicopters Inc.

P. 0. Box 51112 Tulsa, Oklahoma 94151 6 W^c- Civil Air

•~Sle&u£a&&n&'.

4H1?

liughes 769A, 269A-1, 269B . Replacement of Hughes P/N 269A5501 Idler Pulley with Hughes P/N 269A5414 Idler Pulley in accordance with Charles A. Presley Modification Instructions dnted 6-20-73.

approval should not be extended to other aircraft of the models listed hereon on which other approved modif icationa were revloualy incorporated unless it is determined by the Installer that the interrelationship between this change and any other previous modifications have no adverse effect upon the airworthiness of this aircraft. All Air^or thine ss Directives and Manufacturers Service Bulletins applicable to the Hughes P/N ?69Ab414 Idler Pulley when installed on the Hughes Model 269C helicopter are applicable to this part installed on the models covered by this STC.

, June 20, 1973 March 20, 1974 J974 *9rOriginal Signed By Jtmiam 3. Thiavop WILLIAM J.

Chief, Engineering & Manufacturing Branch (Title) ~~~ '_ Any alteration of tkis certificate u punishable by a fine of not exceeding SI ,000, or imprisonment not exceeding 3 years, or both.

fhis certificate may be Iraiaftrred in accordana with I-AR 21.47.

FAAFot* 81 10-2 |10-68)

INSTRUCTIONS: 'I'ho transfer endorse men I below may be used lo notify the appropriate FAA Regional Office of the transfer of lliis Supplemental Type Certificate.

The FAA will reissue the certificate in the name nf the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number ___ to (Name of transferee) (Address of transferee) ! { Nu'nbeT and ftrfrt) ICitf, Slate, and ^IP mde) from (Name of grantor) (Print or type) (Address of grantor) (.Vurnbrr anil Itrtet) (Citf, Slate, and ZIP codr) Extent of Authority (if licensing agreement):

Signature of grantor (In ink): _ 1 C FAA AC G9-5536

## Every issue (1)

- April 8, 1974: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c8/33/c8330ae84780bff15531237ea0a99e97f9657b3d4a15b6e5b3bc8407eff3ce2f)

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